Table 1
List of models.
| id | i d2 | i s2 | q (AU) | nd |
|
|
M 12 | M 21 | e d1 | e d2 | i d1 | i d2 |
|
|
||||||||||||
| a | 45° | 0° | 55 | 2 | − 16% | − 3% | 11% | 10% | 0.09 | 0.09 | 2.6° | − 3.4° |
| b | 45° | 0° | 65 | 2 | − 11% | − 1% | 7% | 6% | 0.05 | 0.05 | 1.0° | − 1.8° |
| c | 45° | 60° | 55 | 2 | − 2% | − 17% | 3% | 13% | 0.04 | 0.07 | 8.5° | 2.0° |
| d | 0° | 0° | 55 | 2 | − 6% | − 5% | 8% | 11% | 0.08 | 0.09 | 0.0° | 0.0° |
| e | ... | 0° | 55 | 1 | − 21% | ... | 15% | 0% | 0.08 | 0.31 | 0.0° | 0.0° |
| f | 180° | 0° | 55 | 2 | − 24% | 2% | 8% | 2% | 0.07 | 0.17 | 0.0° | 0.0° |
| g | 60° | 30° | 55 | 2 | − 10% | − 8% | 9% | 11% | 0.06 | 0.05 | 9.2° | 58.9° |
| h | − 60° | 30° | 55 | 2 | − 17% | 2% | 10% | 5% | 0.06 | 0.06 | 6.0° | 61.6° |
Notes. Each simulation is labeled with a letter in Col. 1; id2 is the mutual inclination between the two disks defined by a rotation along the x-axis; is2 is the inclination of the hyperbolic trajectory of the second star computed with respect to the initial plane of the primary disk; q is the minimum approach distance during the flyby; and nd indicates the number of disks included in the simulation. At the end of each simulation we computed the amount of mass lost by disk 1 and disk 2. M12 and M21 are the amounts of mass transferred from one disk to the other. ed1, ed1, id1, and id1 are the disk eccentricities and inclinations.
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